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Volume & Issue no: Volume 7, Issue 6, June 2018

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Title:
DESIGN AIRCRAFT WING (NACA SERIES) BY USING ANSYS
Author Name:
Amol kumar singh, Vipin Kumar, Er Rahul Malik, Sanjay Bhandari
Abstract:
ABSTRACT The aim of this study is to analyze the modal and theoretical analysis of Aircraft Wing. Aeroelastic phenomena arise when structural deformations induce changes on aerodynamic forces. The additional aerodynamic forces from some sort of perturbation cause increase in the structural deformations, which lead to greater aerodynamic forces. Aeroelasticity is the science which studies the interaction among aerodynamics, inertia and elastic forces. Helping Hand- Atharva Sathaye Index Terms-K method , PK methods, NACA airfoils, ANSYS Workbench
Cite this article:
Amol kumar singh, Vipin Kumar, Er Rahul Malik, Sanjay Bhandari , " DESIGN AIRCRAFT WING (NACA SERIES) BY USING ANSYS" , International Journal of Application or Innovation in Engineering & Management (IJAIEM) , Volume 7, Issue 6, June 2018 , pp. 136-140 , ISSN 2319 - 4847.
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